The invention relates to an electronic arrangement for an aircraft (1), an aircraft having a structure and such an electronic arrangement (3) and a method for providing such an electronic arrangement (3). The electronic arrangement has a structural portion (5) of a structure of an aircraft (1) and one or more structural elements (15), each having a frame (16) and one or more electronic components (20a-c, 26, 27), which are fixed to the frame (16). The structural portion (5) has a reinforcement arrangement (8) of elongate longitudinal and transverse reinforcement elements (6, 7) connected to each other, an outer skin (9), which is arranged on one side of the reinforcement arrangement (8) and is fixed to the longitudinal and transverse reinforcement elements (6, 7), wherein a surface of the outer skin (9) facing away therefrom forms an outer surface (11) of the structural portion (5), and has one or more skin panels (12), each of which is a section of the outer skin (9), which is defined between two directly adjacent longitudinal reinforcement elements (6) of the longitudinal reinforcement elements (6) and two directly adjacent transverse reinforcement elements (7) of the transverse reinforcement elements (7). In at least one of the skin panels (12), an opening (13), completely arranged in the skin panel (12), is formed in the outer skin (9), and for each of the skin panels (12) with one of the openings (13) an associated structural element (15) is separately provided, which is designed and detachably fastened by the frame (16) thereof to the outer skin (9) in the corresponding skin panel (12) on the side of the outer skin (9) opposite the outer surface (11), such that it seals the corresponding opening (13) such that the skin panel (12) has at least the same pressure-tightness and at least the same strength relative to tension, pressure and shear forces which act in the skin panel (12) in the extension direction of the outer skin (9) as the same skin panel (12) without the corresponding opening (13).

    本发明涉及一种用于飞行器(1)的电子布置、一种具有结构和这种电子布置(3)的飞行器、以及一种用于设置这种电子布置(3)的方法。所述电子布置具有飞行器(1)的结构的结构部分(5)和一个或多个结构元件(15),该一个或多个结构元件各自具有框架(16)和一个或多个电子部件(20a‑c,26,27),该一个或多个电子部件固定至所述框架(16)。所述结构部分(5)具有连接至彼此的长形纵向加强元件和横向加强元件(6,7)的加强布置(8),并且具有外蒙皮(9),所述外蒙皮布置在所述加强布置(8)的一侧、并且固定至所述纵向加强元件和所述横向加强元件(6,7),其中,所述外蒙皮(9)的背向所述纵向加强元件和所述横向加强元件的表面形成所述结构部分(5)的外表面(11),并且所述结构部分具有一个或多个蒙皮面板(12),所述一个或多个蒙皮面板中的每个蒙皮面板是所述外蒙皮(9)的、限定在所述纵向加强元件(6)中的两个直接相邻的纵向加强元件(6)之间并且在所述横向加强元件(7)中的两个直接相邻的横向加强元件(7)之间的一部分。在所述蒙皮面板(12)中的至少一个蒙皮面板中,在所述外蒙皮(9)中形成完全布置在所述蒙皮面板(12)中的开口(13),并且对于具有所述开口(13)中的一个开口的所述蒙皮面板(12)中的每一个蒙皮面板,单独地设置有相关联的结构元件(15),所述结构元件被设计并且通过所述结构元件的框架(16)在所述外蒙皮(9)的与所述外表面(11)相反的一侧紧固至所述相应的蒙皮面板(12)中的所述外蒙皮(9),使得所述结构元件密封所述相应的开口(13),使得与不具有所述相应的开口(13)的相同的蒙皮面板(12)相比,所述蒙皮面板(12)具有至少相同的压力密封性和相对于作用在所述蒙皮面板(12)中的所述外蒙皮(9)的延伸方向上的张力、压力、以及剪切力的至少相同的强度。


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    Title :

    ELECTRONIC ARRANGEMENT FOR AIRCRAFT AND METHOD FOR PROVIDING SUCH ELECTRONIC ARRANGEMENT


    Additional title:

    飞行器的电子布置以及提供这种电子布置的方法


    Contributors:

    Publication date :

    2021-12-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / H01Q Antennen , ANTENNAS, i.e. RADIO AERIALS



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